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gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:category
|
gptkb:aircraft
gptkb:helicopter
civil utility aircraft
|
|
gptkbp:countryOfOrigin
|
gptkb:Italy
gptkb:United_States
|
|
gptkbp:crew
|
2
|
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gptkbp:cruiseSpeed
|
509 km/h
|
|
gptkbp:developedBy
|
gptkb:Bell_Helicopter
gptkb:Agusta
|
|
gptkbp:emptyWeight
|
4,800 kg
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney_Canada_PT6C-67A
2
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:FAATypeCertificate
|
pending
|
|
gptkbp:firstAppearance
|
2001 Paris Air Show
|
|
gptkbp:firstFlight
|
2003
|
|
gptkbp:firstPrototypeCrashed
|
2015
|
|
gptkbp:formerName
|
gptkb:Bell/Agusta_BA609
|
|
gptkbp:height
|
4.6 m
|
|
gptkbp:intendedUse
|
search and rescue
medical evacuation
VIP transport
offshore transport
|
|
gptkbp:length
|
13.4 m
|
|
gptkbp:manufacturer
|
gptkb:Leonardo_S.p.A.
|
|
gptkbp:marketedAs
|
gptkb:Leonardo_Helicopters
|
|
gptkbp:maximumSpeed
|
509 km/h
|
|
gptkbp:maxTakeoffWeight
|
7,620 kg
|
|
gptkbp:notableFeature
|
vertical takeoff and landing
tilting rotors
|
|
gptkbp:numberOfPrototypes
|
at least 4
|
|
gptkbp:range
|
1,390 km
|
|
gptkbp:role
|
gptkb:helicopter
civil tiltrotor
|
|
gptkbp:seatingCapacity
|
9
|
|
gptkbp:serviceCeiling
|
7,620 m
|
|
gptkbp:status
|
in development
|
|
gptkbp:successor
|
gptkb:Bell_XV-15
|
|
gptkbp:testFlightsResumed
|
2016
|
|
gptkbp:wingspan
|
12.8 m
|
|
gptkbp:bfsParent
|
gptkb:Paris_Air_Show
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Leonardo AW609
|